Knowledge of flow field behind lifting surfaces of supersonic airplane or missile is important in handling various stability problems; downwash and sidewash angles were measured with conical probe in vertical planes 0.5, 1.0 and 1.5 chord lengths downstream of rectangular wing of biconvex section.


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    Title :

    Measurement of downwash and sidewash behind rectangular wing at mach number of 1.6


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Davis, T. (author)


    Publication date :

    1952


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English